View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 26086U 00009A 25322.54209681 .00000435 00000-0 51600-4 0 9998
2 26086 64.8531 5.4073 0024240 268.7362 91.0977 14.97022851406705
| Epoch (UTC): | 18 November 2025 13:00:37 |
| Eccentricity: | 0.0024240 |
| inclination: | 64.8531° |
| perigee height: | 559 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 5.4073° |
| argument of perigee: | 268.7362° |
| revolutions per day: | 14.97022851 |
| mean anomaly at epoch: | 91.0977° |
| orbit number at epoch: | 40670 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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